DE3885495T2 - Kühlung des Randes einer Düsenklappe. - Google Patents

Kühlung des Randes einer Düsenklappe.

Info

Publication number
DE3885495T2
DE3885495T2 DE88630066T DE3885495T DE3885495T2 DE 3885495 T2 DE3885495 T2 DE 3885495T2 DE 88630066 T DE88630066 T DE 88630066T DE 3885495 T DE3885495 T DE 3885495T DE 3885495 T2 DE3885495 T2 DE 3885495T2
Authority
DE
Germany
Prior art keywords
support plate
coolant
edge
nozzle
cover
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
DE88630066T
Other languages
German (de)
English (en)
Other versions
DE3885495D1 (de
Inventor
Alfredo Cires
George D Lee
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RTX Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE3885495D1 publication Critical patent/DE3885495D1/de
Publication of DE3885495T2 publication Critical patent/DE3885495T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Continuous Casting (AREA)
DE88630066T 1987-04-14 1988-04-13 Kühlung des Randes einer Düsenklappe. Expired - Fee Related DE3885495T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/038,074 US4747542A (en) 1987-04-14 1987-04-14 Nozzle flap edge cooling

Publications (2)

Publication Number Publication Date
DE3885495D1 DE3885495D1 (de) 1993-12-16
DE3885495T2 true DE3885495T2 (de) 1994-02-24

Family

ID=21897953

Family Applications (1)

Application Number Title Priority Date Filing Date
DE88630066T Expired - Fee Related DE3885495T2 (de) 1987-04-14 1988-04-13 Kühlung des Randes einer Düsenklappe.

Country Status (6)

Country Link
US (1) US4747542A (zh)
EP (1) EP0287499B1 (zh)
JP (1) JP2617761B2 (zh)
KR (1) KR950003751B1 (zh)
CN (1) CN1012833B (zh)
DE (1) DE3885495T2 (zh)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2637016A1 (fr) * 1988-09-28 1990-03-30 Snecma Tuyere d'ejection bidimensionnelle de turboreacteur et son systeme de commande
US4934600A (en) * 1988-12-14 1990-06-19 General Electric Company Exhaust nozzle thermal distortion control device
US5101624A (en) * 1989-09-07 1992-04-07 General Electric Company Exhaust nozzle hinge
US5079912A (en) * 1990-06-12 1992-01-14 United Technologies Corporation Convergent side disk cooling system for a two-dimensional nozzle
US5080284A (en) * 1990-06-25 1992-01-14 United Technologies Corporation Cooling system for the trailing edge of a liner
US5131222A (en) * 1990-11-28 1992-07-21 The United States Of Americas As Represented By The Secretary Of The Air Force Thermally valved cooling system for exhaust nozzle systems
US5720434A (en) * 1991-11-05 1998-02-24 General Electric Company Cooling apparatus for aircraft gas turbine engine exhaust nozzles
DE4138784A1 (de) * 1991-11-26 1993-05-27 Mtu Muenchen Gmbh Einrichtung zur abdichtung eines spaltes
US6000635A (en) * 1995-10-02 1999-12-14 Lockheed Martin Corporation Exhaust nozzle for a turbojet engine
DE10303088B4 (de) 2002-02-09 2015-08-20 Alstom Technology Ltd. Abgasgehäuse einer Wärmekraftmaschine
US7188477B2 (en) * 2004-04-21 2007-03-13 United Technologies Corporation High temperature dynamic seal for scramjet variable geometry
US7624567B2 (en) * 2005-09-20 2009-12-01 United Technologies Corporation Convergent divergent nozzle with interlocking divergent flaps
US8205454B2 (en) * 2007-02-06 2012-06-26 United Technologies Corporation Convergent divergent nozzle with edge cooled divergent seals
US7757477B2 (en) * 2007-02-20 2010-07-20 United Technologies Corporation Convergent divergent nozzle with slot cooled nozzle liner
US8051663B2 (en) 2007-11-09 2011-11-08 United Technologies Corp. Gas turbine engine systems involving cooling of combustion section liners
CN105067988B (zh) 2015-07-02 2018-03-30 英特尔公司 集成电路、集成电路测试装置以及方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1355190A (en) * 1970-09-26 1974-06-05 Secr Defence Seals
US3831396A (en) * 1971-08-19 1974-08-27 Aeronautical Res Ass Of Prince Self-regulating thermal protection system for heated surfaces
US4081137A (en) * 1977-01-05 1978-03-28 The United States Of America As Represented By The Secretary Of The Air Force Finned surface cooled nozzle
JPS55103163A (en) * 1979-01-30 1980-08-07 Tokyo Kousou Kk Metal seal of valve
US4410163A (en) * 1982-02-01 1983-10-18 Keystone International, Inc. Valve seat
US4544098A (en) * 1982-12-27 1985-10-01 United Technologies Corporation Cooled exhaust nozzle flaps
US4575006A (en) * 1983-06-13 1986-03-11 United Technologies Corporation Nozzle flap edge seal
JPH0660740B2 (ja) * 1985-04-05 1994-08-10 工業技術院長 ガスタービンの燃焼器

Also Published As

Publication number Publication date
KR880012883A (ko) 1988-11-29
JPS63263251A (ja) 1988-10-31
JP2617761B2 (ja) 1997-06-04
US4747542A (en) 1988-05-31
EP0287499A2 (en) 1988-10-19
CN88102318A (zh) 1988-11-02
DE3885495D1 (de) 1993-12-16
EP0287499B1 (en) 1993-11-10
CN1012833B (zh) 1991-06-12
EP0287499A3 (en) 1990-08-16
KR950003751B1 (ko) 1995-04-18

Similar Documents

Publication Publication Date Title
DE3885495T2 (de) Kühlung des Randes einer Düsenklappe.
DE3875365T2 (de) Gekuehlte auskleidung einer duesenklappe.
DE3811614C1 (zh)
DE69526615T2 (de) Wandaufbau für die Austrittsdüse eines Überschall-Strahltriebwerks
EP1320661B1 (de) Gasturbinenschaufel
DE69503616T2 (de) Doppelte kühlluftversorgung des deckbandes einer turbinenleitschaufel
DE69000424T2 (de) Hitzebestaendige struktur fuer einen nachbrenner oder fuer ein gasturbinenzwischenstueck.
DE2903656C2 (de) Vorrichtung zur Aufprallkühlung der Dichtsegmente einer Turbine eines Turbinenstrahltriebwerks
DE2406277C2 (de) Kühllufteinlaß
DE2657405A1 (de) Oberflaechenkuehlvorrichtung, insbesondere fuer gasturbinentriebwerke
DE3143394A1 (de) Wandaufbau fuer eine brennkammer
DE69504101T2 (de) Strömungsleitplatte zur kühlung der stirnwand einer turbinenbrennkammer
DE69104006T2 (de) Kühleinrichtung für eine Brennkammerwand.
DE1092255B (de) Verfahren zur Kuehlung von Maschinenteilen, insbesondere von hohlen Gasturbinenschaufeln
DE3346809A1 (de) Axialsymmetrische schubduese mit veraenderbarer querschnittsflaeche
DE2155107A1 (de) Gasturbine mit einem Übergangsteil
DE3921894A1 (de) Hyperschall-scramjet-triebwerk und dafuer vorgesehene brennstoffeinspritzvorrichtung
EP0031174B1 (de) Gekühlte Gasturbinenschaufel
DE1280618B (de) Doppelwandige Leitschaufel fuer Gasturbinentriebwerke
DE2043162A1 (de) Lufteinlaß fur die Brennkammer eines Gasturbinentriebwerks
DE69220548T2 (de) System zum Abtransport der Heizflüssigkeit aus einer Anti-Vereisung-Vorrichtung in die Luftzuführung eines Turbostrahltriebwerkes bei niedrigem Druck und mit einem hohen Mischgrad
DE2742296A1 (de) Einrichtung zur verbindung eines einteiligen auspuffsammelrohres mit den zylinderkoepfen mehrzylindriger, reihenfoermiger verbrennungsmotoren
DE2122005A1 (de) Schubumkehrvomchtung fur Gastur binenstrahltnebwerke
CH643050A5 (de) Gasturbinentriebwerk mit ringbrennkammer.
DE1601628C3 (de) Doppelwandige Leitschaufel fur Gas turbinentriebwerke

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee